Turbines compared

首頁

首頁
翱翔天際
Mercury HP
Pegasus HP
Olympus HP
Titan
Nike
Optional Equipment
Olympus university
Turbines compared
Complete package
Version 2 ECU

Specifications

Mercury HP Pegasus HP Olympus HP Titan Nike
Engine diameter. 100 mm 3.9 inches 120 mm 4.7 inches 130 mm 5.1 inches 147 mm 5.8 inches 201 mm 7.9 inches
Engine length. (Airstart engine) 220 mm 8.7 inches 264 mm 10.4 inches 267 mm 10.5 inches 268 mm 10.5 inches N.A. N.A.
Engine length. (Electric start engine) 292 mm 11.5 inches 342 mm 13.4 inches 374 mm 4.7 inches 385 mm 15.1 inches 524 mm 20.6 inches
Engine weight. (Airstart engine) 1400 g 3.1 Lbs 2125 g 4.6 Lbs 2475 g 5.4 Lbs 2975 g 6.6 Lbs N.A. N.A.
Engine weight. (Electric start engine) 1550 g 3.4 Lbs 2255 g 4.9 Lbs 2850 g 6.3 Lbs 3350 g 7.4 Lbs 8770 g 19.3 Lbs
System airborne weight. (Air start system) 
Engine,ECU,pump,battery,thermosensor,straps.
2005 g 4.4 Lbs 2705 g 5.9 Lbs 3150 g 6.9 Lbs 4200 g 9.3 Lbs N.A. N.A.
System airborne weight. (E-start system) 
Engine,ECU,pump,battery,thermosensor,straps.
2235 g 5.1 Lbs 3075 g 6.75 Lbs 3795 g 8.35 Lbs 4575 g 10 Lbs 10580 g 23.3 Lbs
Thrust @ S.T.P. * (*see below) 
15 Deg. Celsius / 1013  Mbar. 
59 Deg. Fahrenheit / 29,91 in.
88N / 9Kp
@ 151,200
19,8 Lbf
@ 151,200
167N / 17,0Kp 
@119,500
37,5 Lbf  
@ 119,500
230N / 23.5Kp 
@108,500
51.7 Lbf 
@108,500
392N / 40Kp 
@96,000
88,2 Lbf 
@96,000
784 N 
@60,000
176.2 Lbf 
@60,000
Maximum allowed r.p.m. 151,900  120,000 112,000 100,000 60,000
Thrust @ idle rpm 4 N 0.9 Lbf 6 N 1.3 Lbf 8 N 1.8 Lbf 13 N 2.9 Lbf 40 N 9 Lbf
Idle rpm 47,600  37,000 36,000 30,000 20,000
Pressure ratio @ max. rpm 2.8 : 1 3.2 : 1 3.8 : 1 3.8 : 1 4 : 1
Mass flow 250 g/sec
@88 N
0.55 Lb/sec
@19,8 Lbf
375 g/sec
@157 N
0.85 Lb/sec
@35,3 Lbf
450 g/sec
@230 N
0.99 Lb/sec
@51.7 Lbf
660 g/sec
@392 N
1.46 Lb/sec
@88.2 Lbf
1100 g/sec
@784 N
2.42 Lb/sec
@176.2 Lbf
Normal Exhaust Gas Temperature. 650 C 1200 F 600 C 1110 F 700 C 1290 F 740 C 1364 F 760 C 1400 F
Maximum Exhaust Gas Temperature. 750 C 1380 F 675 C 1250 F 750 C 1380 F 780 C 1436 F 800 C 1472 F
Fuel Consumption
@ max. r.p.m. and S.T.P. * (*see below)
290 g/min
@88 N
10 oz/min
@19,8 Lbf
450 g/min
@157 N
15.7 oz/min
@35,3 Lbf
640 g/min
@230 N
22.5 oz/min
@51.7 Lbf
1120g/min
@392 N
39.5 oz/min
@88.2Lbf
1740g/min
@784 N
61.37 oz/min
@176.2Lbf
Fuel types. Kerosene - Paraffin - Jet A1 -  White Spirit
* S.T.P. Standard Temp. & Pressure 
Temp: 15° Celcius / 59° Fahrenheit 
Pressure: 1013 Mbar / 29.91 in
 
Suitable oils for our range of turbines are: AeroShell 500
AeroShell 560
Mobil Jet oil II
 
All specifications are subject to change without notice.

 

 


[首頁] [翱翔天際] [Mercury HP] [Pegasus HP] [Olympus HP] [Titan] [Nike] [Optional Equipment] [Olympus university] [Turbines compared] [Complete package] [Version 2 ECU]

新 北 市 汐 止 區 康 寧 街 169 巷 23 號 7 樓 之 一

公司電話:+886-2-2695-8906(代表號)

 02-2695-6755, 02-2695-7011, 02-2695-7033

公司傳真:+886-2-26958911

利偉 分機:21  jaco@bentech-taiwan.com

上次更新日期: 2016年09月06日。